Stringer assemblies and methods of forming thereof
AssigneeThe Boeing Company
InventorsForouzan Behzadpour, Waeil M. Ashmawi
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AssigneeThe Boeing Company
InventorsForouzan Behzadpour, Waeil M. Ashmawi
Estimating the term…
Described herein are stringer assemblies, such as blade stringers, and methods of forming thereof. A stringer assembly comprises a first fabric composite stiffener, a second fabric composite stiffener, and an intermediate tape composite stiffener, disposed between and connected to each of the first and second stiffeners. Using three separate components allows forming sharp bends, eliminating voids and gap fillers, and adding new features, such as edge reinforcements. Each of the first and second fabric composite stiffeners comprises a web portion, a flange portion, and a curved portion, positioned between the web and flange portions. The web portions surround and are attached to the intermediate tape composite stiffener and, in some examples, include tapered-out edges for additional rigidity. The flange portions are attached to the composite base. The curved portions conform to the flared-out edges of the intermediate tape composite stiffener, which extends and connects to the composite base.
A stringer assembly comprising:
A method of forming a stringer assembly, the method comprising:
A method for forming a stringer assembly, the method comprising:
A method for forming a stringer assembly, the method comprising:
Dependencies are inferred from the claim text.